|Publication number||US7879286 B2|
|Application number||US 11/448,160|
|Publication date||Feb 1, 2011|
|Filing date||Jun 7, 2006|
|Priority date||Jun 7, 2006|
|Also published as||CN101501228A, CN101501228B, EP2038443A1, EP2038443A4, US20070286761, WO2007142837A1|
|Publication number||11448160, 448160, US 7879286 B2, US 7879286B2, US-B2-7879286, US7879286 B2, US7879286B2|
|Inventors||Daniel B. Miracle, Seshacharyulu Tamirisakandala, Radhakrishna B. Bhat, Dale J. McEldowney, Jerry L. Fields, William M. Hanusiak, Rob L. Grabow, C. Fred Yolton, Eric S. Bono|
|Original Assignee||Miracle Daniel B, Seshacharyulu Tamirisakandala, Bhat Radhakrishna B, Mceldowney Dale J, Fields Jerry L, Hanusiak William M, Grabow Rob L, Yolton C Fred, Bono Eric S|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (5), Non-Patent Citations (4), Referenced by (8), Classifications (10), Legal Events (2)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The present invention may be manufactured and used by or for the Government of the United States for all governmental purposes without the payment of any royalty.
1. Field of the Invention
The present invention relates generally to methods for enhancing the performance of conventional titanium alloys without a reduction in damage tolerance and, more specifically, to a method for producing homogeneous microstructure in the broad family of titanium alloys including, but not limited to Ti-6 wt. % Al-4 wt. % V, Ti-5Al-2.5Sn, Ti-6Al-2Sn-4Zr-2Mo-O.1Si.
2. Description of the Background Art
Titanium alloys offer attractive physical and mechanical property combinations that make them suitable for a variety of structural applications in various industries (e.g. aerospace) to obtain significant weight savings and reduced maintenance costs compared to other metallic materials such as steels. There have been several efforts to further increase the strength and stiffness of conventional titanium alloys to obtain enhanced performance. These approaches involve addition of particulates, short fibers, or continuous fibers that possess high strength and stiffness. Although these prior art approaches increase the strength and stiffness of conventional titanium alloys significantly, the increases are obtained with an accompanying drastic reduction in ductility and damage tolerance owing to the presence of brittle reinforcement, which restricts their usage in fracture-sensitive applications. A value of 5% tensile elongation is often considered in structural applications to separate ductile from brittle behavior.
Accordingly, a purpose of the present invention is to provide a novel methodology for producing titanium alloys with significant enhancement in strength and stiffness relative to conventional titanium alloys while maintaining adequate ductility. The method described herein involves addition of a small amount of boron below a critical level, and deforming the alloy at a specified range of temperature and deformation rate, to obtain uniform microstructure.
In accordance with the new and improved method of the present invention, the strength and stiffness of titanium alloys are increased, while maintaining ductility, by the addition of boron and controlled processing to obtain uniform microstructure.
Important features of the present method are as follows:
1. The boron concentration in the titanium alloy should be at or below the eutectic limit so that it does not possess any coarse primary TiB particles;
2. The titanium alloys containing boron are heated above the beta transus temperature (temperature at which the titanium alloy transforms fully to high temperature body-centered cubic beta phase) to completely force out any supersaturated boron (boron trapped inside the lattice of titanium under non-equilibrium solidification conditions); and
3. The boron-modified titanium alloy is subjected to deformation at a slow rate, e.g., extrusion at slow speed, to avoid damage to the TiB micro-constituent which reduces ductility.
The present invention provides a novel method of increasing the strength and stiffness while maintaining the ductility of titanium alloys by the addition of boron and controlled processing. This new and improved method causes the natural evolution of fine and uniform microstructural features. Although the description hereinafter is specific to a powder metallurgy processing technique, the invention is equally applicable to other metallurgical processing techniques.
In the pre-alloyed powder metallurgy approach, the boron is added to the molten titanium alloy and the melt is atomized to obtain boron-containing titanium alloy powder. The powder may be consolidated and/or formed via conventional techniques such as hot isostatic pressing, forging, extrusion and rolling.
The method of the present invention includes four important elements which are described hereinafter.
1) Boron Level at or Below the Eutectic Limit
While boron is fully soluble in liquid titanium, its solubility in the solid phase is negligible. The binary Titanium-Boron phase diagram shown in
2) Carbon Level Below a Critical Limit
It has been discovered that the carbon concentration also significantly influences the ductility of boron-modified titanium alloys and it is important to keep the carbon level below below a critical limit to avoid an unacceptable loss of ductility. Unlike boron, the solid solubility of carbon in titanium is high (up to 0.5 weight %) and carbon in titanium could cause embrittlement. The carbon concentration, therefore, should be controlled depending on the alloy composition and processing parameters to achieve acceptable ductility values. For example,
3) Thermal Exposure Above the Beta Transus
Owing to negligible solid solubility of boron in titanium, excess boron is trapped (supersaturated) inside the lattice of titanium under non-equilibrium solidification conditions (e.g. powder manufacture via rapid solidification techniques such as gas atomization). Titanium alloy with supersaturated boron is inherently brittle and possesses low ductility values. It has been discovered that the supersaturated boron can be forced out via thermal exposure at a high temperature. Experiments to determine the optimum temperature for eliminating the supersaturation are illustrated in
Thermal exposure at lower temperatures results in close inter-particle spacing which restricts the ductility. Exposure above the beta transus increases the inter-particle spacing which improves the ductility. The rate at which the material is cooled after thermal exposure alters the grain size and morphology, both of which also significantly influence the ductility. Controlled slow cooling from above the beta transus produces fine-grained equiaxed alpha-beta microstructure due to the influence of TiB particles on the phase transformation reaction of high temperature beta to room temperature alpha. The beta transus varies with the composition of principal alloying elements in conventional titanium alloys, and, e.g., is 1850±50° F. for Ti-6Al-4V. Thermal exposure may be applied via hot isostatic pressing, extrusion, or another suitable consolidation method, or by thermal treatment before or after consolidation, or thermo-mechanical processing. The effects of thermal treatments in HIP compacts and extrusions are shown in
4) Deformation Rate Control to Avoid Microstructural Damage
The rate at which boron-modified titanium alloy is subjected to deformation also has significant influence on the final microstructure and mechanical properties. Microstructures of Ti-6Al-4V-1B-0.1C material extruded at a fast ram speed (100 inch/mm) and slow speed (15 inch/mm) are shown in
The properties of slow-speed extruded Ti-64-1B are compared with a typical Ti-6Al-4V alloy  in
It will be readily seen, therefore, that the new and improved method of the present invention increases the strength and stiffness of conventional titanium alloys without significant loss in ductility, thus significantly enhancing the structural performance of titanium alloys.
Boron-modified titanium alloys could be produced using traditional processing methods and conventional metalworking (e.g. forging, extrusion, rolling) equipment can be used to perform controlled processing. Therefore, the improved performance with the use of the present method is obtained without any increase in material or processing cost.
Titanium alloys with 25-35% increases in strength and stiffness could replace existing expensive components for high performance and could enable new structural design concepts for weight and cost reduction.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiments, it is to be understood that the invention is not to be limited to the disclosed embodiments, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
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|Citing Patent||Filing date||Publication date||Applicant||Title|
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|US8499605||Jul 28, 2010||Aug 6, 2013||Ati Properties, Inc.||Hot stretch straightening of high strength α/β processed titanium|
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|US8652400||Jun 1, 2011||Feb 18, 2014||Ati Properties, Inc.||Thermo-mechanical processing of nickel-base alloys|
|US8834653||Jul 2, 2013||Sep 16, 2014||Ati Properties, Inc.||Hot stretch straightening of high strength age hardened metallic form and straightened age hardened metallic form|
|US9050647||Mar 15, 2013||Jun 9, 2015||Ati Properties, Inc.||Split-pass open-die forging for hard-to-forge, strain-path sensitive titanium-base and nickel-base alloys|
|US9192981||Mar 11, 2013||Nov 24, 2015||Ati Properties, Inc.||Thermomechanical processing of high strength non-magnetic corrosion resistant material|
|U.S. Classification||419/12, 148/513, 148/671|
|Cooperative Classification||C22C14/00, B22F9/082, C22F1/183|
|European Classification||C22F1/18B, C22C14/00, B22F9/08D|
|Dec 6, 2010||AS||Assignment|
Owner name: ATI PROPERTIES, INC., OREGON
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:YOLTON, C. FRED;BONO, ERIC S.;SIGNING DATES FROM 20101130 TO 20101203;REEL/FRAME:025451/0534
|Aug 1, 2014||FPAY||Fee payment|
Year of fee payment: 4